[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 15th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
292/16:06:53
238 -2
9 5
6 5
6
N/A -4
4 0
0 214
8
000/00:01:46
476 -1
9 0
0 204
7
299/12:44:03
843 -5
1 6
7 6
7
N/A -4
3 -0
0 217
0
000/00:02:07
687 0
3 0
0 205
3
Coasting Arc #1 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2011/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1391140
94 A = 6766683
54 meter
Y = -5933055
10 meter E =
0016100
Z = -2917295
26 I = 51
30513
XDOT = 4641
795196 Wp = 343
31724
YDOT = -3542
446746 meter/sec RA = 279
35197 deg
ZDOT = 4999
294859 TA = 343
09360
MA = 343
14719
Ha = 213
546 n
mi
Hp = 203
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4564110
70 X = -1310520
96
Y = -19465403
88 feet Y = -5948161
10 meter
Z = -9571178
68 Z = -2923857
37
XDOT = 15228
986864 XDOT = 4656
776343
YDOT = -11622
200609 feet/sec YDOT = -3490
455270 meter/sec
ZDOT = 16401
886019 ZDOT = 5021
881796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11440259
33 X = 3486991
04
Y = 16381316
35 feet Y = 4993025
22 meter
Z = -9597575
58 Z = -2925341
04
XDOT = -8510
136499 XDOT = -2593
889605
YDOT = 15590
907930 feet/sec YDOT = 4752
108737 meter/sec
ZDOT = 16494
036450 ZDOT = 5027
382310
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11287
50595049
00016717 00000-0 10270-3 0 9003
2 25544 51
6380 280
0903 0016181 327
1312 32
8837 15
60680174 19541
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50595049 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 280
0903 deg
Eccentricity:
0016181
Arg of perigee: 327
1312 deg
Mean anomaly: 32
8837 deg
Mean motion: 15
60680174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 298
Coasting Arc #2 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2011/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1152566
29 A = 6769868
53 meter
Y = 6625623
93 meter E =
0006380
Z = -811416
80 I = 51
31226
XDOT = -4634
220872 Wp = 347
75961
YDOT = -1532
311127 meter/sec RA = 274
32361 deg
ZDOT = -5914
778402 TA = 201
06791
MA = 201
09420
Ha = 213
732 n
mi
Hp = 203
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3781385
47 X = -1222627
86
Y = 21737611
32 feet Y = 6612343
46 meter
Z = -2662128
60 Z = -817186
56
XDOT = -15204
136719 XDOT = -4588
008311
YDOT = -5027
267477 feet/sec YDOT = -1583
875703 meter/sec
ZDOT = -19405
440952 ZDOT = -5937
179593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4982878
52 X = -1518781
37
Y = -21491068
21 feet Y = -6550477
59 meter
Z = -2685974
60 Z = -818685
06
XDOT = 14287
594994 XDOT = 4354
858954
YDOT = -870
024973 feet/sec YDOT = -265
183612 meter/sec
ZDOT = -19496
565097 ZDOT = -5942
553042
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11288
53043913
00016717 00000-0 10270-3 0 9016
2 25544 51
6377 274
9311 0016207 331
0848 28
9409 15
60744909 19705
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53043913 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 274
9311 deg
Eccentricity:
0016207
Arg of perigee: 331
0848 deg
Mean anomaly: 28
9409 deg
Mean motion: 15
60744909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 315
Coasting Arc #3 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3253595
09 A = 6762615
58 meter
Y = -4247206
38 meter E =
0012319
Z = 4125443
21 I = 51
28717
XDOT = 3070
182128 Wp = 13
70069
YDOT = 5972
262660 meter/sec RA = 269
28121 deg
ZDOT = 3736
679983 TA = 37
79574
MA = 37
70929
Ha = 213
685 n
mi
Hp = 203
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10674524
58 X = 3280805
33
Y = -13934404
15 feet Y = -4210670
42 meter
Z = 13534918
66 Z = 4141315
70
XDOT = 10072
776012 XDOT = 2985
018465
YDOT = 19594
037600 feet/sec YDOT = 6006
119258 meter/sec
ZDOT = 12259
448762 ZDOT = 3751
388157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4049237
00 X = -1234207
44
Y = 17028124
29 feet Y = 5190172
28 meter
Z = 13599771
32 Z = 4145210
30
XDOT = -15830
056341 XDOT = -4825
001173
YDOT = -13578
359922 feet/sec YDOT = -4138
684104 meter/sec
ZDOT = 12319
019549 ZDOT = 3754
837158
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11289
55489364
00016717 00000-0 10270-3 0 9024
2 25544 51
6375 269
7724 0016210 334
1444 25
8901 15
60808021 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55489364 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 269
7724 deg
Eccentricity:
0016210
Arg of perigee: 334
1444 deg
Mean anomaly: 25
8901 deg
Mean motion: 15
60808021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 317
Coasting Arc #4 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2011/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4246500
45 A = 6757981
15 meter
Y = -35020
40 meter E =
0016721
Z = -5263829
43 I = 51
27325
XDOT = -439
517258 Wp = 31
96054
YDOT = -7649
853816 meter/sec RA = 264
19227 deg
ZDOT = 420
032920 TA = 241
97801
MA = 242
14726
Ha = 213
883 n
mi
Hp = 202
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13932088
11 X = -4220222
09
Y = -114896
31 feet Y = -82360
56 meter
Z = -17269781
58 Z = -5284395
43
XDOT = -1441
985754 XDOT = -355
982898
YDOT = -25097
945592 feet/sec YDOT = -7654
301692 meter/sec
ZDOT = 1378
060760 ZDOT = 418
100797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12595795
38 X = 3839198
43
Y = -5706383
14 feet Y = -1739305
58 meter
Z = -17353523
17 Z = -5289353
86
XDOT = 11447
902743 XDOT = 3489
320756
YDOT = 21245
700564 feet/sec YDOT = 6475
689532 meter/sec
ZDOT = 1370
592418 ZDOT = 417
756569
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11290
51529107
00016717 00000-0 10270-3 0 9033
2 25544 51
6375 264
9358 0016169 338
3256 21
7214 15
60823753 20019
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51529107 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 264
9358 deg
Eccentricity:
0016169
Arg of perigee: 338
3256 deg
Mean anomaly: 21
7214 deg
Mean motion: 15
60823753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 296
Coasting Arc #5 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2011/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763044
69 A = 6764156
38 meter
Y = 4331952
38 meter E =
0017625
Z = 3590716
76 I = 51
29870
XDOT = -2462
671830 Wp = 23
03630
YDOT = 5792
747773 meter/sec RA = 259
10968 deg
ZDOT = -4384
414046 TA = 114
14201
MA = 113
95761
Ha = 214
031 n
mi
Hp = 202
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12345947
14 X = 3696880
98
Y = 14212442
21 feet Y = 4373663
20 meter
Z = 11780566
79 Z = 3608837
05
XDOT = -8079
631987 XDOT = -2505
965474
YDOT = 19005
077994 feet/sec YDOT = 5764
966499 meter/sec
ZDOT = -14384
560519 ZDOT = -4396
483155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17241937
44 X = -5255342
53
Y = -7442630
90 feet Y = -2268513
90 meter
Z = 11854135
01 Z = 3613140
35
XDOT = -1631
573388 XDOT = -497
303569
YDOT = -19330
629901 feet/sec YDOT = -5891
975994 meter/sec
ZDOT = -14434
004865 ZDOT = -4399
484683
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11291
53968026
00016717 00000-0 10270-3 0 9044
2 25544 51
6374 259
7766 0016260 341
8910 18
1665 15
60897410 20179
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53968026 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 259
7766 deg
Eccentricity:
0016260
Arg of perigee: 341
8910 deg
Mean anomaly: 18
1665 deg
Mean motion: 15
60897410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 317
Coasting Arc #6 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2011/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1849032
60 A = 6769571
08 meter
Y = -6495197
31 meter E =
0024549
Z = 5044
73 I = 51
32408
XDOT = 4625
332496 Wp = 11
14251
YDOT = -1308
294650 meter/sec RA = 254
07531 deg
ZDOT = 6005
023026 TA = 348
91232
MA = 348
96632
Ha = 214
011 n
mi
Hp = 202
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6066379
91 X = -1776289
10
Y = -21309702
45 feet Y = -6515467
59 meter
Z = 16550
97 Z = -3761
07
XDOT = 15174
975381 XDOT = 4610
446724
YDOT = -4292
305281 feet/sec YDOT = -1256
654400 meter/sec
ZDOT = 19701
519115 ZDOT = 6027
456998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15029433
11 X = 4580971
21
Y = 16279448
31 feet Y = 4961975
85 meter
Z = -18986
73 Z = -5787
16
XDOT = -10312
320315 XDOT = -3143
195232
YDOT = 9527
398635 feet/sec YDOT = 2903
951104 meter/sec
ZDOT = 19792
947106 ZDOT = 6032
890278
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11292
50001400
00016717 00000-0 10270-3 0 9057
2 25544 51
6373 254
9400 0016061 345
7207 14
3493 15
60954520 20321
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
50001400 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 254
9400 deg
Eccentricity:
0016061
Arg of perigee: 345
7207 deg
Mean anomaly: 14
3493 deg
Mean motion: 15
60954520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 262
Coasting Arc #7 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/292/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2997335
76 A = 6762275
51 meter
Y = 3607573
21 meter E =
0017749
Z = -4880837
02 I = 51
29477
XDOT = -3796
672796 Wp = 12
44756
YDOT = -6261
571519 meter/sec RA = 253
22417 deg
ZDOT = -2281
074486 TA = 235
06628
MA = 235
23315
Ha = 214
846 n
mi
Hp = 204
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9833778
75 X = -3013743
13
Y = 11835870
11 feet Y = 3573963
27 meter
Z = -16013244
83 Z = -4895438
19
XDOT = -12456
275576 XDOT = -3715
291334
YDOT = -20543
213644 feet/sec YDOT = -6303
573283 meter/sec
ZDOT = -7483
840178 ZDOT = -2299
321024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11652302
49 X = -3551621
80
Y = -9954955
80 feet Y = -3034270
53 meter
Z = -16072888
27 Z = -4899016
35
XDOT = 20044
478796 XDOT = 6109
557137
YDOT = -11177
752765 feet/sec YDOT = -3406
979043 meter/sec
ZDOT = -7557
839509 ZDOT = -2303
629482
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11292
69208254
00016717 00000-0 10270-3 0 9064
2 25544 51
6409 253
9740 0015903 330
5447 29
4811 15
59934199 20351
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69208254 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 253
9740 deg
Eccentricity:
0015903
Arg of perigee: 330
5447 deg
Mean anomaly: 29
4811 deg
Mean motion: 15
59934199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 319
Coasting Arc #8 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/293/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4499938
81 A = 6761363
50 meter
Y = 373758
31 meter E =
0017561
Z = 5039534
08 I = 51
30179
XDOT = 1403
649404 Wp = 351
45928
YDOT = 7329
495439 meter/sec RA = 248
13881 deg
ZDOT = -1780
670121 TA = 115
93188
MA = 115
75080
Ha = 214
888 n
mi
Hp = 204
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14763578
79 X = 4470943
58
Y = 1226241
18 feet Y = 423917
50 meter
Z = 16533904
47 Z = 5061324
51
XDOT = 4605
148962 XDOT = 1330
235464
YDOT = 24046
901045 feet/sec YDOT = 7344
781345 meter/sec
ZDOT = -5842
093574 ZDOT = -1774
029797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1247005
75 X = -380087
35
Y = 14661851
15 feet Y = 4468932
23 meter
Z = 16622635
79 Z = 5066579
39
XDOT = -22983
736036 XDOT = -7005
442744
YDOT = 4698
561995 feet/sec YDOT = 1432
121696 meter/sec
ZDOT = -5815
401721 ZDOT = -1772
534445
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11293
71708077
00016717 00000-0 10270-3 0 9077
2 25544 51
6405 248
8186 0015948 333
8482 26
1867 15
60000396 20516
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
71708077 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 248
8186 deg
Eccentricity:
0015948
Arg of perigee: 333
8482 deg
Mean anomaly: 26
1867 deg
Mean motion: 15
60000396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 317
Coasting Arc #9 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2011/294/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620505
95 A = 6768632
81 meter
Y = -4000397
38 meter E =
0016680
Z = -2885431
62 I = 51
33897
XDOT = 1685
687935 Wp = 353
61663
YDOT = -5563
322841 meter/sec RA = 243
07781 deg
ZDOT = 5027
228682 TA = 333
23922
MA = 333
32519
Ha = 214
990 n
mi
Hp = 204
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15159140
25 X = -4561412
28
Y = -13124663
33 feet Y = -4051736
48 meter
Z = -9466639
19 Z = -2907734
43
XDOT = 5530
472228 XDOT = 1723
351246
YDOT = -18252
371526 feet/sec YDOT = -5544
261538 meter/sec
ZDOT = 16493
532422 ZDOT = 5035
509662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12884249
97 X = 3927119
39
Y = -15307769
50 feet Y = -4665808
14 meter
Z = -9557294
27 Z = -2913063
29
XDOT = 17219
030101 XDOT = 5248
360375
YDOT = 4201
473995 feet/sec YDOT = 1280
609274 meter/sec
ZDOT = 16527
521435 ZDOT = 5037
588533
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11294
67798761
00016717 00000-0 10270-3 0 9083
2 25544 51
6408 243
9854 0015891 337
5007 22
5450 15
60016555 20666
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
67798761 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 243
9854 deg
Eccentricity:
0015891
Arg of perigee: 337
5007 deg
Mean anomaly: 22
5450 deg
Mean motion: 15
60016555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 323
Coasting Arc #10 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2011/295/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3128190
16 A = 6772042
61 meter
Y = 5977723
17 meter E =
0006899
Z = -635867
25 I = 51
36514
XDOT = -4519
389344 Wp = 15
91878
YDOT = 1733
528030 meter/sec RA = 238
05634 deg
ZDOT = -5945
551687 TA = 170
98034
MA = 170
96795
Ha = 215
168 n
mi
Hp = 204
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10263091
09 X = 3064202
55
Y = 19611952
65 feet Y = 6012346
68 meter
Z = -2086178
65 Z = -620826
26
XDOT = -14827
392862 XDOT = -4509
555377
YDOT = 5687
427919 feet/sec YDOT = 1683
043948 meter/sec
ZDOT = -19506
403174 ZDOT = -5967
483365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19261652
37 X = -5870951
64
Y = 10917840
91 feet Y = 3327757
91 meter
Z = -2025182
55 Z = -617275
64
XDOT = -5373
186570 XDOT = -1637
747266
YDOT = -13108
913488 feet/sec YDOT = -3995
596831 meter/sec
ZDOT = -19595
816479 ZDOT = -5972
804863
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11295
70292147
00016717 00000-0 10270-3 0 9096
2 25544 51
6408 238
8300 0015695 340
9380 19
1186 15
60034271 20820
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
70292147 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 238
8300 deg
Eccentricity:
0015695
Arg of perigee: 340
9380 deg
Mean anomaly: 19
1186 deg
Mean motion: 15
60034271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 300
Coasting Arc #11 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2011/296/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -300504
94 A = 6765644
23 meter
Y = -5533963
11 meter E =
0015345
Z = 3863470
02 I = 51
36124
XDOT = 5996
616571 Wp = 27
73273
YDOT = 2526
378489 meter/sec RA = 233
02465 deg
ZDOT = 4091
980057 TA = 19
33309
MA = 19
27494
Ha = 215
279 n
mi
Hp = 203
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -985908
61 X = -257369
06
Y = -18156046
94 feet Y = -5537081
99 meter
Z = 12675426
57 Z = 3862115
44
XDOT = 19673
938881 XDOT = 5948
042029
YDOT = 8288
643335 feet/sec YDOT = 2593
165116 meter/sec
ZDOT = 13425
131419 ZDOT = 4120
993818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18079139
48 X = 5510521
71
Y = -1972922
75 feet Y = -601346
86 meter
Z = 12670153
37 Z = 3861862
75
XDOT = -7438
668938 XDOT = -2267
306292
YDOT = 18665
818137 feet/sec YDOT = 5689
341368 meter/sec
ZDOT = 13543
207397 ZDOT = 4127
969615
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11296
72782033
00016717 00000-0 10270-3 0 9109
2 25544 51
6408 233
6734 0015853 345
2823 14
7869 15
60096744 20989
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
72782033 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 233
6734 deg
Eccentricity:
0015853
Arg of perigee: 345
2823 deg
Mean anomaly: 14
7869 deg
Mean motion: 15
60096744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 322
Coasting Arc #12 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2011/297/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2904615
11 A = 6759804
85 meter
Y = 3081393
97 meter E =
0019906
Z = -5279890
80 I = 51
36150
XDOT = -5305
003746 Wp = 35
98425
YDOT = -5530
803875 meter/sec RA = 227
95199 deg
ZDOT = -294
146325 TA = 231
11241
MA = 231
29014
Ha = 215
260 n
mi
Hp = 203
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9529577
15 X = -2913206
72
Y = 10109560
26 feet Y = 3048864
26 meter
Z = -17322476
37 Z = -5294022
85
XDOT = -17404
867933 XDOT = -5241
333984
YDOT = -18145
682004 feet/sec YDOT = -5589
771709 meter/sec
ZDOT = -965
046999 ZDOT = -319
763379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10720922
73 X = -3267737
25
Y = -8722120
68 feet Y = -2658502
38 meter
Z = -17380180
19 Z = -5297478
92
XDOT = 16295
804006 XDOT = 4966
961061
YDOT = -17800
373621 feet/sec YDOT = -5425
553880 meter/sec
ZDOT = -1069
161443 ZDOT = -325
880408
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11297
68863015
00016717 00000-0 10270-3 0 9116
2 25544 51
6406 228
8396 0015834 348
2385 11
8398 15
60188376 21138
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
68863015 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 228
8396 deg
Eccentricity:
0015834
Arg of perigee: 348
2385 deg
Mean anomaly: 11
8398 deg
Mean motion: 15
60188376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 328
Coasting Arc #13 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2011/298/16:07:46
476
Vector Time (MET): N/A
Weight (LBS) : 870922
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5314953
13 A = 6764016
83 meter
Y = 390659
21 meter E =
0019882
Z = 4171222
93 I = 51
39814
XDOT = 2443
524668 Wp = 22
36474
YDOT = 6274
825016 meter/sec RA = 222
87576 deg
ZDOT = -3677
348285 TA = 105
57317
MA = 105
35361
Ha = 215
284 n
mi
Hp = 202
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17437510
27 X = 5289926
12
Y = 1281690
33 feet Y = 449954
66 meter
Z = 13685114
60 Z = 4196982
79
XDOT = 8016
813215 XDOT = 2391
041066
YDOT = 20586
696248 feet/sec YDOT = 6301
856279 meter/sec
ZDOT = -12064
790962 ZDOT = -3665
605306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 189547
41 X = 57774
05
Y = 17400882
65 feet Y = 5303789
03 meter
Z = 13790040
27 Z = 4203204
27
XDOT = -18559
514265 XDOT = -5656
939948
YDOT = 9787
256576 feet/sec YDOT = 2983
155804 meter/sec
ZDOT = -12017
224517 ZDOT = -3662
850033
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11298
71346090
00016717 00000-0 10270-3 0 9121
2 25544 51
6411 223
6834 0015876 351
6458 8
4431 15
60264726 21290
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
71346090 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 223
6834 deg
Eccentricity:
0015876
Arg of perigee: 351
6458 deg
Mean anomaly: 8
4431 deg
Mean motion: 15
60264726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 305
Coasting Arc #14 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:45:07
687
Vector Time (MET): N/A
Weight (LBS) : 870297
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3275159
38 A = 6763292
03 meter
Y = 2745620
93 meter E =
0016555
Z = -5247302
85 I = 51
40289
XDOT = -5571
736578 Wp = 29
47278
YDOT = -5218
939842 meter/sec RA = 218
55742 deg
ZDOT = 762
047414 TA = 247
74075
MA = 247
91639
Ha = 217
014 n
mi
Hp = 205
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10745273
56 X = -3280126
88
Y = 9007942
68 feet Y = 2708968
05 meter
Z = -17215560
54 Z = -5263226
22
XDOT = -18279
975651 XDOT = -5516
665245
YDOT = -17122
506044 feet/sec YDOT = -5280
938456 meter/sec
ZDOT = 2500
155559 ZDOT = 735
113211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1146888
64 X = 349571
66
Y = -13894118
93 feet Y = -4234927
45 meter
Z = -17280554
55 Z = -5267113
03
XDOT = 24029
990523 XDOT = 7324
341112
YDOT = -928
109266 feet/sec YDOT = -282
887704 meter/sec
ZDOT = 2390
651114 ZDOT = 728
670460
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11299
54611559
00016717 00000-0 10270-3 0 9139
2 25544 51
6407 219
4941 0017175 337
7207 22
3200 15
59027652 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54611559 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 219
4941 deg
Eccentricity:
0017175
Arg of perigee: 337
7207 deg
Mean anomaly: 22
3200 deg
Mean motion: 15
59027652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 298
Coasting Arc #15 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2011/300/12:45:07
687
Vector Time (MET): N/A
Weight (LBS) : 870297
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5595701
79 A = 6768708
61 meter
Y = 55074
30 meter E =
0018761
Z = 3817683
94 I = 51
44535
XDOT = 2789
731868 Wp = 18
23282
YDOT = 5812
897345 meter/sec RA = 213
50151 deg
ZDOT = -4149
829352 TA = 115
65849
MA = 115
46458
Ha = 217
148 n
mi
Hp = 204
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18358601
67 X = 5576123
91
Y = 180689
95 feet Y = 117539
47 meter
Z = 12525209
77 Z = 3844821
06
XDOT = 9152
663608 XDOT = 2744
683248
YDOT = 19071
185515 feet/sec YDOT = 5843
841877 meter/sec
ZDOT = -13614
925695 ZDOT = -4136
385992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12825858
19 X = -3909321
58
Y = 13030206
54 feet Y = 3971606
95 meter
Z = 12635777
10 Z = 3851384
86
XDOT = -19185
357418 XDOT = -5847
696941
YDOT = -5661
928071 feet/sec YDOT = -1725
755676 meter/sec
ZDOT = -13560
408937 ZDOT = -4133
212644
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11300
57170300
00016717 00000-0 10270-3 0 9140
2 25544 51
6402 214
3433 0017129 341
4937 18
5593 15
59064306 21587
Satellite: ISS
Catalog Number: 25544
Epoch time: 11300
57170300 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 214
3433 deg
Eccentricity:
0017129
Arg of perigee: 341
4937 deg
Mean anomaly: 18
5593 deg
Mean motion: 15
59064306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 281
Coasting Arc #16 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2011/301/12:45:07
687
Vector Time (MET): N/A
Weight (LBS) : 870297
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6196357
05 A = 6774501
98 meter
Y = -2542096
31 meter E =
0024368
Z = -905647
68 I = 51
49141
XDOT = 1096
219224 Wp = 4
36453
YDOT = -4771
842551 meter/sec RA = 208
48278 deg
ZDOT = 5928
309210 TA = 345
77529
MA = 345
84378
Ha = 217
199 n
mi
Hp = 204
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20329255
40 X = -6163070
71
Y = -8340211
00 feet Y = -2611201
65 meter
Z = -2971285
03 Z = -935669
51
XDOT = 3596
519764 XDOT = 1120
698052
YDOT = -15655
651415 feet/sec YDOT = -4759
447140 meter/sec
ZDOT = 19449
833367 ZDOT = 5933
694196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19950724
76 X = 6080980
91
Y = -9168700
47 feet Y = -2794619
90 meter
Z = -3093508
20 Z = -942901
30
XDOT = 8409
328024 XDOT = 2563
163182
YDOT = 11764
977521 feet/sec YDOT = 3585
965149 meter/sec
ZDOT = 19471
991473 ZDOT = 5935
063001
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11301
53316095
00016717 00000-0 10270-3 0 9151
2 25544 51
6406 209
5139 0017179 344
7307 15
3328 15
59115055 21738
Satellite: ISS
Catalog Number: 25544
Epoch time: 11301
53316095 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 209
5139 deg
Eccentricity:
0017179
Arg of perigee: 344
7307 deg
Mean anomaly: 15
3328 deg
Mean motion: 15
59115055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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